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Materials Testing

Sample of Reinforced Carbon Carbon (RCC) material. RCC is a graphite reinforced carbon composite matrix coated with a silicone carbide conversion with sodium silicate sealant and can withstand temperatures up to 3600 degrees F. Sample of Reinforced Carbon Carbon (RCC) material. RCC is a graphite reinforced carbon composite matrix coated with a silicone carbide conversion with sodium silicate sealant and can withstand temperatures up to 3600 degrees F. CAIB Photo by Rick Stiles 2003 View
Sample of an actual Reinforced Carbon Carbon (RCC) T-seal cross-section shows the rounded “locking” side and flat “sliding” side of the seal. CAIB Photo by Rick Stiles 2003 Sample of an actual Reinforced Carbon Carbon (RCC) T-seal cross-section shows the rounded “locking” side and flat “sliding” side of the seal. CAIB Photo by Rick Stiles 2003 View
Scott Hubbard, CAIB board member, inspects damaged RCC panel #8 following test. CAIB Photo by Rick Stiles 2003 Scott Hubbard, CAIB board member, inspects damaged RCC panel #8 following test. CAIB Photo by Rick Stiles 2003 View
Scott Hubbard, CAIB board member, inspects damaged RCC panel #8 following test.CAIB Photo by Rick Stiles 2003 Scott Hubbard, CAIB board member, inspects damaged RCC panel #8 following test.
CAIB Photo by Rick Stiles 2003 View
Air Gun at Southwest Research Institute (SwRI) in San Antonio, TX used for shuttle External Tank foam insulation impact tests. Air Gun at Southwest Research Institute (SwRI) in San Antonio, TX used for shuttle External Tank foam insulation impact tests. The large blue tank on the left is pressurized with nitrogen which when released fires a foam projectile through the long brown horizontal barrel. In this test, the barrel is aimed for an impact point on reinforced carbon carbon (RCC) panel #8 on the left wing test article. CAIB Photo by Rick Stiles 2003 View
Left wing test article prior to foam impact test. Panels 5, 6, and 7 and T-Seals 5/6 and 6/7 (from left) are made of fiberglass. Left wing test article prior to foam impact test. Panels 5, 6, and 7 and T-Seals 5/6 and 6/7 (from left) are made of fiberglass. The target panel #8 and outboard panels (continuing to the right) are actual flight Reinforced Carbon Carbon (RCC) material including T-Seals 8/9, 9/10, and 10/11. The black ‘skid’ marks on fiberglass panel 6 are from earlier foam impact tests in the series used to gather data in preparation for actual RCC impact tests. CAIB Photo by Rick Stiles 2003 View
Wing leading edge test article after impact test clearly shows an approximate 16 inch hole in RCC panel 8. This is the 'after' photo from the image above. CAIB Photo by Rick Stiles 2003 Wing leading edge test article after impact test clearly shows an approximate 16 inch hole in RCC panel 8. This is the ‘after’ photo from the image above. CAIB Photo by Rick Stiles 2003 View
 
 

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Updated September 17, 2009
Steve Garber, NASA History Web Curator
Jennifer Troxell, Author
For further information, e-mail histinfo@hq.nasa.gov
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edited by Lisa Jirousek
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